Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and DevelopmentPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Active Control Systems - Review, Evaluation and Projections
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and DevelopmentPublisher:
ISBN:
Category :
Languages : en
Pages :
Book Description
Active Control Systems
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Flight Mechanics PanelPublisher:
ISBN:
Category : Control theory
Languages : en
Pages : 400
Book Description
Scientific and Technical Aerospace Reports
Author: Conference Proceedings of Active Control Systems - Review, Evaluation and Projections Presented at Toronto, Canada on 15-18 October 1984
Author: ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT NEUILLY-SUR-SEINE (France)Publisher:
ISBN:
Category :
Languages : en
Pages : 383
Book Description
Active Control Technology was the subject of this symposium, as it was of a previous FMP/GCP symposium held in 1974. At that time, Active Control could only be viewed in the future - and the view presented at that symposium was very optimistic. Ten years and numerous applications of Active Control Technology later, the view of Active Control which emanated from this symposium was still very optimistic. Certainly some of the projections for significantly reduced tail sizes have been revised in the light of the realities of getting hung-up at high angle of attack with little stability and no control. While the substantial performance benefits projected in 1974 have been modestly lowered based on our intervening experience, the potential of such advanced Active Control configurations as the X-29 is yet to be established. The ability to manage properly multiple redundant flight control systems, which was a major concern in 1974, is still a concern but tempered by several significant successes. Also the dissimilar backup flight control systems to counter undetected design faults has not been demonstrated. Active Control Technology provided the impetus for disregarding those allegedly outmoded Flying Qualities Specifications (a common 1974 view), so that full advantage could be taken of the high-gain, full-authority system with simulation-tailored control laws. In reality, one of the most significant benefits of Active Control Technology was to allow easy revision of the control laws when our flight experiences underlined the need for meeting those outmoded Flying Qualities Specifications.
Active Control Systems--review, Evaluation and Projections
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Flight Mechanics Panel. SymposiumPublisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 422
Book Description
The papers considered comprehensive range of topics including: Active Control Technology applications; optimisation of systems architecture for both reliability and cost; control low design, development and test; the application of handling qualities criteria and the operational demonstration ofsystem reliability.
NASA Technical Paper
Author: United States. National Aeronautics and Space AdministrationPublisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 168
Book Description
AGARD Advisory Report
Author: North Atlantic Treaty Organization. Advisory Group for Aerospace Research and DevelopmentPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 32
Book Description
Linearized Aerodynamic and Control Law Models of the X-29A Airplane and Comparison with Flight Data
Author: John T. BosworthPublisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 120
Book Description
Scientific and Technical Information Output of the Langley Research Center for Calendar Year 1984
Author: Control and Dynamic Systems V52: Integrated Technology Methods and Applications in Aerospace Systems Design
Author: C.T. LeonidesPublisher: Elsevier
ISBN: 032316319X
Category : Transportation
Languages : en
Pages : 563
Book Description
Control and Dynamic Systems: Advances in Theory and Applications, Volume 52: Integrated Technology Methods and Applications in Aerospace System Design discusses the various techniques and applications in aerospace systems. This book presents automation and integration techniques in optimizing aircraft structural design. It also covers a number of technologies used in aerospace systems such as active flutter suppression, flight control configuration, aeroassisted plane change missions, flight control systems, and impaired aircraft. This book concludes by demonstrating some modeling issues in command, control, and communication networks. This book is a significant reference source for engineers involved in aerospace systems design.